Indian Martian exploration program

Varoon2

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A discovery revealed from Mangalyaan , which is still going strong 7 years and 5 months after launch

 

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Copied content from above link in case link expires.
Feb 28, 2022
Indian Mars Orbiter Mission (MOM) used for Investigating the Solar Corona by ISRO Scientists
Utilizing the solar conjunction event, when the Earth and Mars are on the opposite sides of the Sun, a team of scientists from Space Physics Laboratory of Vikram Sarabhai Space Centre, Trivandrum; Physical Research Laboratory, Ahmedabad; and ISRO Telemetry Tracking and Command Network (ISTRAC), Bangalore; used S-band radio signals coming from the Indian Mars Orbiter Mission (MOM) to study the Solar Corona. During conjunction events, which usually happens once in approximately two years for Mars, the radio signals from MOM passes through the solar corona, as close as 10 solar radii (1 solar radii (Rʘ) = 696,340 km = about 100 Earth radii), from the center of the Sun, thus providing a unique opportunity to study solar dynamics. ISRO scientists used the conjunction event of May-June 2015 – a time when the Sun's activity was quite low, to study the turbulence in the solar corona and found that transition of solar wind from sub-alfvenic to super-alfvenic flow occurs around 10–15 Rʘ during low solar activity period.
The outer atmosphere of the Sun, called the solar corona, is the region where the temperature is several million degrees Kelvin, rendering it quite inaccessible for in-situ measurements thereby challenging the experimenters. The reason for such a high temperature of the corona is still an enigma. The solar wind, which originates in the corona and accelerates in this region, passes through the interplanetary spaces, shapes the magnetosphere of planets, as well as affects the near-Earth space environment through a phenomenon known as "Space Weather".
Since the solar corona is an ionized medium (plasma) and has its intrinsic turbulence, it is a dispersive medium for an electromagnetic radio wave passing through it. The radio signals from MOM spacecraft crossing through the solar corona during the conjunction event (cf. Figure 1) consequently experience dispersive effects. The turbulence in the corona produces fluctuations in plasma density which get registered as fluctuations in the phase of radio waves passing through it. Thus, the radio signals received at the ground station (Indian Deep Space Network, ISTRAC for MOM) contain the signature of propagating medium (solar corona) and can be spectrally analyzed to derive the turbulence spectrum of the medium. This forms the basis of the coronal radio-sounding technique which has been used by spacecraft to study coronal regions spanning maximum and minimum phases of different solar cycles.

ISRO scientists obtained coronal turbulence spectrum at heliocentric distances between 4 and 20 Rʘ by spectrally analyzing the Doppler frequency residuals from radio signals received from MOM spacecraft. This is the region where the solar wind primarily gets accelerated to velocities of a few hundreds of kilometers per second. The changes in turbulence regime are well reflected in spectral index values of the temporal frequency fluctuation spectrum. The scientists found that the turbulence power spectrum at a lower heliocentric distance (<10 Rʘ) has flattened at shorter frequencies with a smaller spectral index, which corresponds to the solar wind acceleration region. Smaller spectral index values closer to the Sun’s surface signify the energy input regime where turbulence is still underdeveloped. For larger heliocentric distances (> 10 Rʘ), the curve steepens with a spectral index close to 2/3, which is indicative of the inertial regime of a developed Kolmogorov-type turbulence, where energy is transported through cascading. This finding is consistent with those of theoretical models of solar wind turbulence and substantiates the process of turbulence energy transport and dissipation of magnetohydrodynamic waves, leading to coronal heating and solar wind acceleration in the near-Sun region.

Incidentally, this finding of ISRO scientists is also supported by the first direct observation of solar corona by Parker Probe, published very recently in an independent study.

Another intriguing observation is when the results of studies by MOM are compared with similar experiments conducted by the earlier missions which spanned past solar cycles. The work based on MOM data reports an insight into the feeble maxima of solar cycle 24, which is recorded as a peculiar solar cycle in terms of overall lower activity than any other previous solar cycle.

These outstanding science results on the solar coronal dynamics using MOM in an innovative way is published in the refereed journal Monthly Notices of the Royal Astronomical Society, titled "A study on the solar coronal dynamics during the post-maxima phase of the solar cycle 24 using S-band radio signals from the Indian Mars Orbiter Mission", authored by Richa N. Jain,R. K. Choudhary, Anil Bhardwaj, Umang Parikh, Bijoy K. Dai, and Roopa M. V.

Monthly Notices of the Royal Astronomical Society, DOI: 10.1093/mnras/stac056

https://academic.oup.com/mnras/advance-article-abstract/doi/10.1093/mnras/stac056/6506470

PS: - India’s first mission to Mars, the MOM, was launched on 5 November 2013, and arrived at Mars on 24 September 2014. The MOM was planned for a mission lifetime of 6 months, but has successfully surpassed it by a factor of 10 now in Martian orbit for more than 7 years, and is doing well in the extended mission phase. The MOM has provided the first measurements of the evening time exosphere of Mars (1) and has discovered hot Argon in its upper atmosphere-exosphere by the MENCA experiment onboard MOM (2).

(1) MENCA observed the evening exosphere of Mars

(2) Observation of Suprathermal Argon in Mars Exosphere

 Schematic of positions of Earth and MOM spacecraft relative to the Ecliptic plane of Sun (XY plane) as seen from Earth.  Radio signals sent by spacecraft (dashed line) pass closer to the solar coronal region during this period.

Figure 1. Schematic of positions of Earth and MOM spacecraft relative to the Ecliptic plane of Sun (XY plane) as seen from Earth. Radio signals sent by spacecraft (dashed line) pass closer to the solar coronal region during this period.
 

Varoon2

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I'm pretty sure it's September 24th in India :), and that means the Mangalyaan/Mars Orbiter has now been in orbit around Mars for 8 straight years! It entered the Martin orbit around this time on Sept 24th/2014. ISRO should give an update on its status, and its expected further duration.
 

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New Mars Mission Still In "Study Phase," Says ISRO Scientist
The Mars mission has to be bigger with a more scientific outcome, M Sankaran, Director, of UR Rao Satellite Centre of the Indian Space Research Organisation (ISRO) told PTI.
New Mars Mission Still In Study Phase, Says ISRO Scientist

India successfully launched its first Mars Orbiter Mission called Mangalyaan.
Bengaluru: The second mission to Mars is in the study phase as the Indian space agency is looking at various options available to make the mission happen, a senior ISRO scientist said on Thursday.
The Mars mission has to be bigger with a more scientific outcome, M Sankaran, Director, of UR Rao Satellite Centre of the Indian Space Research Organisation (ISRO) told PTI.
"If you are talking about a new mission to Mars, then that is still in the study phase. We are looking at various options available to us for making a mission happen. It has to be significantly bigger or with more scientific outcomes with respect to Mars Orbiter Mission (MOM). We are still in the study phase and we are configuring it," Sankaran told PTI.
India successfully launched its first Mars Orbiter Mission called Mangalyaan on November 5, 2013, which started orbiting the red planet on September 24, 2014. The orbiter lost contact in October 2022 and thus the Mangalyaan-1 mission came to an end.
Regarding Chandrayaan-3, he said the lunar spacecraft had already reached the launch port.
"The preparation is going on in Sriharikota. We do expect that sometime in July the launch will take place," he said.
According to the space scientist, every aspect of the mission has been checked, especially those experiences that ISRO gleaned from its Chandrayaan-2 mission.
"All possible precautions have been taken. The mood at ISRO is upbeat," he added.
Regarding India's space mission Gaganyaan, Sankaran said it was an intense project with a lot of new development activities taking place.
"Many developments and many tests are happening, which is not visible to the public. Lots of works are going on. We do expect that there will be something which will be visible to people during this year," he added.
 

Vamsi

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These are the upcoming launch windows for Mars with required delta-V budgets,If we launch before 24th November 2026, then our current LVM-3 can only launch a payload just over 1000Kgs directly into a Mars Transfer Trajectory, hence it can only be Lander & Rover only mission without any orbiter
1694079846243.png




@Indx TechStyle @Swesh @FalconSlayers @Tactical Doge @Marliii @TopWatcher
 

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Mars Orbiter Mission-2
PRL has proposed and developing the following instruments for second Indian Mars Orbiter Mission (MOM-2). These instruments have been selected for MOM-2 and are at various stages of the development.

Mars Orbit Dust Experiment (MODEX)
To understand origin, abundance, distribution and flux at high altitudes on Mars, a MODEX is proposed. There are no measurements of Interplanetary Dust Particles (IDPs) at Mars. The instrument can detect particles of size from few hundreds nm to few µm, travelling at hypervelocity (> 1 km/s). The outcomes can help explain the dust flux at Mars, whether there is any ring (as hypothesized) around Mars and also confirm whether the dust is interplanetary or coming from the Phobos/Deimos. The study of dust can help explain the RO experiment results.

Radio Occultation (RO) Experiment
To measure the neutral and electron density profiles, the RO is proposed. The instrument is microwave transmitter (or receiver as per option) on board, operating at X-band frequency and it can provide the bending angle due to the Martian atmosphere. It can help understand the behaviour of the Martian atmosphere.

Energetic Ion Spectrometer (EIS)
To characterize SEPs and supra-thermal solar wind particles at the Martian environment and to understand their role in the loss of Martian atmosphere. This instrument will measure high-energy charge particles in the energy range of 20 keV to 20 MeV.

Langmuir Probe and Electric Field Experiment (LPEX)
To measure electron number density (Ne), electron temperature (Te), electric field waves in order to understand the Martian plasma environment. LPEX experiment consists of one Langmuir probe (LP) and two electric field (EF) sensors each mounted on a long boom.
 

Swesh

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Mars Orbiter Mission-2
PRL has proposed and developing the following instruments for second Indian Mars Orbiter Mission (MOM-2). These instruments have been selected for MOM-2 and are at various stages of the development.

Mars Orbit Dust Experiment (MODEX)
To understand origin, abundance, distribution and flux at high altitudes on Mars, a MODEX is proposed. There are no measurements of Interplanetary Dust Particles (IDPs) at Mars. The instrument can detect particles of size from few hundreds nm to few µm, travelling at hypervelocity (> 1 km/s). The outcomes can help explain the dust flux at Mars, whether there is any ring (as hypothesized) around Mars and also confirm whether the dust is interplanetary or coming from the Phobos/Deimos. The study of dust can help explain the RO experiment results.

Radio Occultation (RO) Experiment
To measure the neutral and electron density profiles, the RO is proposed. The instrument is microwave transmitter (or receiver as per option) on board, operating at X-band frequency and it can provide the bending angle due to the Martian atmosphere. It can help understand the behaviour of the Martian atmosphere.

Energetic Ion Spectrometer (EIS)
To characterize SEPs and supra-thermal solar wind particles at the Martian environment and to understand their role in the loss of Martian atmosphere. This instrument will measure high-energy charge particles in the energy range of 20 keV to 20 MeV.

Langmuir Probe and Electric Field Experiment (LPEX)
To measure electron number density (Ne), electron temperature (Te), electric field waves in order to understand the Martian plasma environment. LPEX experiment consists of one Langmuir probe (LP) and two electric field (EF) sensors each mounted on a long boom.
Somebody copy pasted this article into Hindustan Times from dfi thinking that MARS mission is ready 😂😂🤣😂 who stealing here these are mere configaration payloads are not ready 😂🤣😂

@Vamsi @Indx TechStyle @FalconSlayers
 

Vamsi

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Somebody

Somebody copy pasted this article into Hindustan Times from dfi thinking that MARS mission is ready 😂😂🤣😂 who stealing here these are mere configaration payloads are not ready 😂🤣😂

@Vamsi @Indx TechStyle @FalconSlayers
Dr. Somanath clearly said that he is dissatisfied with the proposals that came for MOM-2 .....as far as MLM is concerned it seems ISRO might choose Airbags (just like in Spirit & Opportunity rover landing systems) instead of retropropulsion landing (CY-3, Phoenix lander ) to land on Mars , Airbags method is safer & more reliable than retropropulsion landing
 

Vamsi

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Mars Orbiter Mission-2
PRL has proposed and developing the following instruments for second Indian Mars Orbiter Mission (MOM-2). These instruments have been selected for MOM-2 and are at various stages of the development.

Mars Orbit Dust Experiment (MODEX)
To understand origin, abundance, distribution and flux at high altitudes on Mars, a MODEX is proposed. There are no measurements of Interplanetary Dust Particles (IDPs) at Mars. The instrument can detect particles of size from few hundreds nm to few µm, travelling at hypervelocity (> 1 km/s). The outcomes can help explain the dust flux at Mars, whether there is any ring (as hypothesized) around Mars and also confirm whether the dust is interplanetary or coming from the Phobos/Deimos. The study of dust can help explain the RO experiment results.

Radio Occultation (RO) Experiment
To measure the neutral and electron density profiles, the RO is proposed. The instrument is microwave transmitter (or receiver as per option) on board, operating at X-band frequency and it can provide the bending angle due to the Martian atmosphere. It can help understand the behaviour of the Martian atmosphere.

Energetic Ion Spectrometer (EIS)
To characterize SEPs and supra-thermal solar wind particles at the Martian environment and to understand their role in the loss of Martian atmosphere. This instrument will measure high-energy charge particles in the energy range of 20 keV to 20 MeV.

Langmuir Probe and Electric Field Experiment (LPEX)
To measure electron number density (Ne), electron temperature (Te), electric field waves in order to understand the Martian plasma environment. LPEX experiment consists of one Langmuir probe (LP) and two electric field (EF) sensors each mounted on a long boom.
There should be 4 more instruments apart from the above instruments
1. Hyperspectral Imager
2. High Res Pan Cam
3. Dual band SAR
4. ARIS (from IIST) - a retarding potential analyser
 

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